Impact resistant surface insulation tile for a space vehicle and associated protection method

a technology for space vehicles and impact resistance, applied in the field of impact resistance surface insulation tiles for space vehicles, can solve the problems of reducing the mass of these objects, reducing the speed of the rlv, and so as to reduce the maintenance cost, not to unnecessarily increase the weight of the rlv, the effect of increasing the life of the rlv

Inactive Publication Date: 2003-11-20
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

0016] Therefore, the tile of the present invention not only thermally insulates the RLV during flight, but also advantageously protects the RLV from MMOD. In this regard, MMOD that impact upon the tile are fragmented by the tile and captured by the SIP before impacting the RLV, thereby potentially increasing the life of the RLV and reducing maintenance costs. As a result of its construction, the tile is generally lightweight so as not to unnecessarily add to the weight of the RLV. Although the tile of the present invention is most commonly used on an RLV, the superior thermal and impact resistance properties of the invented tile could be utilized in any myriad of applications requiring a low density, highly insulative material.

Problems solved by technology

The impact resistant insulation tiles may completely cover the RLV or may be strategically placed in certain areas that pose a greater risk to the RLV if damaged.
This process not only reduces the mass of these objects, it also reduces their velocity.

Method used

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  • Impact resistant surface insulation tile for a space vehicle and associated protection method
  • Impact resistant surface insulation tile for a space vehicle and associated protection method
  • Impact resistant surface insulation tile for a space vehicle and associated protection method

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Embodiment Construction

[0021] The present invention now will be described more fully with reference to the accompanying drawings, in which preferred embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. Like numbers refer to like elements throughout.

[0022] As previously stated, the RLV experiences extreme temperatures during flight, ranging from -250.degree. F. while in orbit to nearly 2500.degree. F. upon reentry to the atmosphere. Therefore, a thermal protection system is necessary to protect the RLV and critical systems from damage due to these extreme temperatures. It is also desirable to protect the RLV from MMOD. Impact resistant insulation tiles of the present invention provide both thermal and impact pro...

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Abstract

An impact resistant insulation tile is provided that is capable of withstanding the impact of Micrometeriods and Other Debris (MMOD). The tiles are secured to an exterior surface of a Reusable Launch Vehicle (RLV). A durable coating is applied to the exterior surface of a thermally insulative layer to fragment and slow down MMOD that collide with the tile. In addition, a shock layer may be embedded within the thermal insulator to further reduce the size and speed of MMOD particles. A ballistic strain isolator pad may also be located between the thermal insulator and the RLV structure to capture fragmented particles.

Description

FIELD OF THE INVENTION[0001] The present invention relates to tile components that provide both thermal and impact protection for a reusable launch vehicle such as the space shuttle.BACKGROUND OF THE INVENTION[0002] A reusable launch vehicle (RLV), such as the space shuttle, repeatedly travels into or beyond the earth's upper atmosphere and then returns to the earth's surface. During flight, the RLV experiences extreme temperatures, ranging from -250.degree. F. while in orbit to nearly 2500.degree. F. upon reentry to the atmosphere. Because of the extreme temperatures, the vehicle and its contents must be protected by a thermal protection system.[0003] Thermal protection systems for RLVs are constructed from a large number, usually several thousand, of insulation tiles. The tiles function to insulate the vehicle from the environment and to radiate and reflect heat from the vehicle. In addition to protecting the vehicle from environmental heat sources, the insulation tiles also provi...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B64G1/50B64G1/56B64G1/58
CPCB64G1/503B64G1/58B64G1/56
Inventor GUBERT, MICHAEL K.BELL, DANIEL R. IIITRAN, DUOC T.HINKLE, KARRIE ANN
Owner THE BOEING CO
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